Gauss Pseudospectral Method Applied to Multi-Objective Spacecraft Trajectory Optimization

被引:14
|
作者
Zhao, Jiang [1 ,2 ]
Zhou, Rui [2 ]
Jin, Xuelian [3 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[3] Beijing Microelect Technol Inst, Beijing 100076, Peoples R China
基金
中国国家自然科学基金;
关键词
Gauss Pseudospectral Method (GPM); Optimal Control; Spacecraft Trajectory Optimization; Multi-Objective; TRAINS;
D O I
10.1166/jctn.2014.3685
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
The Gauss pseudospectral method (GPM) is used to solve the spacecraft trajectory optimization which includes numerous nonlinear equations of motion and nonlinear constraints. The multi-objective function and geometry path constraints are designed in the optimal control problem. Based on a space entry model, the optimal flight trajectories of a simple spacecraft formation are simulated. The numerical results show that the team objective of the formation is achieved without violating the dynamic capability of each individual spacecraft.
引用
收藏
页码:2242 / 2246
页数:5
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